FAA 8110.42 : 2014
Current
The latest, up-to-date edition.
PARTS MANUFACTURER APPROVAL PROCEDURES
Hardcopy , PDF
English
01-01-2014
CHAPTER 1 - PURPOSE, ADMINISTRATIVE INFORMATION
AND BACKGROUND
CHAPTER 2 - AIRCRAFT CERTIFICATION OFFICE (ACO)
RESPONSIBILITIES
CHAPTER 3 - MANUFACTURING INSPECTION DISTRICT
OFFICE (MIDO) RESPONSIBILITIES
CHAPTER 4 - DESIGNATED ENGINEERING REPRESENTATIVES
AND ORGANIZATION DESIGNATION AUTHORIZATION
APPENDIX A - PMA PROCESS FLOWCHARTS
APPENDIX B - PART SPECIFIC CERTIFICATION PLAN
APPENDIX C - LIST OF FAA MANUFACTURING INSPECTION
DISTRICT/SATELLITE OFFICES
APPENDIX D - SAMPLE FAA-PMA SUPPLEMENT FOR IDENTICALITY
(NON-LICENSING AGREEMENT) OR TEST AND
COMPUTATION
APPENDIX E - SAMPLE DESIGN REJECTION LETTER
APPENDIX F - SAMPLE NOTIFICATION LETTER OF DESIGN
APPROVAL
APPENDIX G - FORM 8110-3, TEST AND COMPUTATION
(GENERAL ANALYSIS)
APPENDIX H - FORM 8110-3, TEST AND COMPUTATION
(COMPARATIVE ANALYSIS)
APPENDIX I - EXAMPLE OF FAA FORM 8110-3 FOR
IDENTICALITY
APPENDIX J - LIST OF ACRONYMS
APPENDIX K - DEFINITIONS AND TERMS
APPENDIX L - RELATED PUBLICATIONS AND HOW TO
GET THEM
APPENDIX M - ADMINISTRATIVE INFORMATION
APPENDIX N - FAA FORM 1320-19 DIRECTIVES FEEDBACK
INFORMATION
Specifies the responsibilities and procedures for approving replacement and modification articles for installation on type-certificated products.
| DevelopmentNote |
Supersedes FAA N 8110.54, FAA N 8110.55 and FAA N 8120.17. (07/2003)
|
| DocumentType |
Standard
|
| Pages |
41
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| Supersedes |
| FAA N 8110.79 : 0 | GUIDELINES FOR THE APPROVAL OF FIELD-LOADABLE SOFTWARE BY FINDING IDENTICALITY THROUGH THE PARTS MANUFACTURER APPROVAL PROCESS |
| FAA 8110.105 : 2017 | SIMPLE AND COMPLEX ELECTRONIC HARDWARE APPROVAL GUIDANCE |
| FAA AC 21-51 : 2011 | APPLICANTS SHOWING OF COMPLIANCE AND CERTIFYING STATEMENT OF COMPLIANCE |
| FAA AC 20-184 : 2015 | GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT |
| FAA AC 33.83-1 : 2009 | COMPARATIVE METHOD TO SHOW EQUIVALENT VIBRATORY STRESSES AND HIGH CYCLE FATIGUE CAPABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS |
| FAA AC 21-55 : 2016 | PROCESS TO SUPPORT FAA FINDINGS OF UNDUE BURDEN OR NO UNDUE BURDEN FOR PAHS REQUESTING TO USE A MANUFACTURING FACILITY LOCATED OUTSIDE OF THE UNITED STATES |
| FAA AC 20-161 : 2008 | AIRCRAFT ONBOARD WEIGHT AND BALANCE SYSTEMS |
| FAA N 8110.110 : 2010 | SOFTWARE APPROVAL GUIDE LINES, CONTINUED |
| FAA IR 01-01 : 0 | AIRCRAFT CERTIFICATION GUIDE FOR THE USE OF ELECTRONIC TECHNOLOGY AND ALTERNATIVE METHODS OF STORING INFORMATION |
| FAA 8110.104 : 2007 | RESPONSIBILITIES AND REQUIREMENTS FOR IMPLEMENTING PART 26 SAFETY INITIATIVES |
| FAA AC 33.19-1 : 2004 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.19, DURABILITY, FOR RECIPROCATING ENGINE REDESIGNED PARTS |
| FAA AC 20-142 : 2010 | ELIGIBILITY AND EVALUATION OF U.S. MILITARY SURPLUS FLIGHT SAFETY CRITICAL AIRCRAFT PARTS, ENGINES, AND PROPELLERS |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| SAE ARP1619B | Replacement and Modified Brakes and Wheels |
| FAA AC 33-8 : 2009 | GUIDANCE FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS UNDER TEST AND COMPUTATION |
| FAA AC 00-56 : 2015 | VOLUNTARY INDUSTRY DISTRIBUTOR ACCREDITATION PROGRAM |
| FAA AC 43-18 : 2011 | FABRICATION OF AIRCRAFT PARTS BY MAINTENANCE PERSONNEL |
| FAA 8110.54 : 2010 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS |
| FAA AC 23-27 : 2009 | PARTS AND MATERIALS SUBSTITUTION FOR VINTAGE AIRCRAFT |
| FAA 8100.15 : 2013 | ORGANIZATION DESIGNATION AUTHORIZATION PROCEDURES |
| FAA AC 21-31 : 2010 | QUALITY CONTROL FOR THE MANUFACTURE OF NON-METALLIC COMPARTMENT INTERIOR COMPONENTS |
| FAA AC 21-23 : 2004 | AIRWORTHINESS CERTIFICATION OF CIVIL AIRCRAFT, ENGINES, PROPELLERS, AND RELATED PRODUCTS IMPORTED TO THE UNITED STATES |
| FAA AC 33.87-2 : 2009 | COMPARATIVE ENDURANCE TEST METHOD TO SHOW DURABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS |
| MIL-STD-1916 Base Document:1996 | DOD Preferred Methods for Acceptance of Product |
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